Avro 652 Anson vs. Lockheed Martin C-130J Super Hercules

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Avro 652 Anson versus Lockheed Martin C-130J Super Hercules
12.88 m 42 ft 3 in length 34.37 m 112 ft 9 in
2.9 m 9 ft 6 in height 11.86 m 38 ft 11 in
17.22 m 56 ft 6 in wingspan 40.41 m 132 ft 7 in
2 × Armstrong Siddeley Cheetah VI engines 4 x Rolls-Royce AE 2100D3 turboprop engines
290 hp (220 kW) thrust per engine Approximately 4,700 hp per engine
580 hp (440 kW) total thrust Approximately 18,800 hp total
7,500 lb 3,402 kg MTOW 76,610 kg 168,900 lb
1,267 km 684 nm range 4,600 km 2,485 nm
165 mph 266 km/h cruise speed 660 km/h 410 mph
4 passengers capacity based on configuration
rotor diameter
rate of climb
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.